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EASA Regulations & Airworthiness Directives

Browse 4995 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320280Airbus A321276Airbus A319246Airbus A350214Airbus A330210All194Airbus A318185Airbus A380171Boeing 737170Airbus A340140Airbus A350-941125Airbus BD-500 (A220 Series)116Airbus Helicopters AS 332116Airbus Helicopters EC 225113Airbus Helicopters SA 330113Show all...

EASA SIB 2020-04

Lithium Batteries used in Emergency Locator Transmitters

EASA Safety Information Bulletin 2020-04 is an airworthiness bulletin addressing lithium batteries used in Emergency Locator Transmitters (ELT) from HR Smith (Technical Developments) Ltd and Techtest Ltd. It applies to specific ELT part numbers including 500-12(), 500-27(), 500-32-2Y, 500-32-2Y-S, 500-32-2Y-S-D, and battery packs A01477 and A0696Y, installed on or carried aboard aircraft certified under CS-23, CS-25, CS-27, and CS-29 or equivalent regulations. The bulletin highlights potential fire risks from thermal runaway in these lithium batteries and provides safety recommendations without mandating regulatory action.

Mar 16, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2020-0056

Engine Fuel & Control — Engine Control Unit — Software Update

EASA Airworthiness Directive 2020-0056 is an official directive addressing the SOLO 2625 02i engine with electronic fuel injection, commonly installed on Binder Motorenbau, DG-Flugzeugbau, and Schempp-Hirth powered sailplanes. This directive mandates an update to the engine control unit (ECU) software to correct a fuel injection error. The update ensures continued airworthiness and safe operation of affected engines.

Mar 13, 2020
Airworthiness DirectiveMaintenanceSafety MgmtSolo Kleinmotoren Gmbh 2625Binder Motorenbau DG-FlugzeugbauSchempp-Hirth

EASA AD 2020-0057

Rotorcraft Flight Manual — Supplements / One Engine Inoperative Performance Limitations — Amendment

The Rotorcraft Flight Manual — Supplements / One Engine Inoperative Performance Limitations — Amendment applies to the AIRBUS HELICOPTERS EC175 model. This amendment updates the flight manual supplements to reflect revised performance limitations when operating with one engine inoperative. It ensures that pilots and operators have the latest performance data for safe and compliant operation of the EC175 rotorcraft.

Mar 13, 2020
OtherFlight OpsSafety MgmtAirbus Helicopters EC175

EASA SD SD-2020-01

SUPERSEDED BY EASA SD-2020-03

EASA Safety Directive 2020-01 is a safety directive issued under Article 76(6)(b) of Regulation (EU) No 2018/1139 addressing operational measures to prevent the spread of the SARS-CoV-2 coronavirus infection. It applies to aircraft operators certified under Commission Regulation (EU) 965/2012 involved in commercial air transport of passengers, focusing on aircraft operating from airports in high-risk areas for COVID-19 transmission. The directive mandates cleaning and disinfection procedures and the carriage of Universal Precaution Kits on affected aircraft.

Mar 13, 2020
Safety DirectiveFlight OpsSafety Mgmt

EASA SD SD-2020-02

SUPERSEDED BY EASA SD-2020-04

EASA Safety Directive 2020-02 is a safety directive issued on 13 March 2020 addressing operational measures to prevent the spread of the Coronavirus SARS-CoV-2 infection. It applies to Third Country Operators authorized by EASA to perform commercial air transport of passengers into, within, or out of the European Union territory. The directive focuses on cleaning and disinfecting aircraft and equipping them with Universal Precaution Kits to protect crew members from potential infection.

Mar 13, 2020
Safety DirectiveFlight OpsSafety Mgmt

EASA SIB NM-20-02

Boeing 737-8 and 737-9 Aeroplanes - Fire Protection

The Special Airworthiness Information Bulletin SAIB: NM-20-02 is an FAA informational bulletin addressing a fire protection concern on Boeing 737-8 and 737-9 airplanes. It highlights a potential issue with the red shipping cap left on the inlet port of electronic equipment bay smoke detectors, specifically part number 2156-756A. The bulletin does not mandate corrective action but provides guidance to operators.

Mar 12, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2020-0050

[Correction] Fuselage — Main Deck Cargo Crossbeams — Inspection / Repair

EASA Airworthiness Directive 2020-0050 is a corrective directive addressing inspection and repair of the main deck cargo crossbeams on Airbus A300-600 aeroplanes, specifically models A300 F4-605R and A300 F4-622R with manufacturer serial numbers 805 to 872 inclusive. The directive mandates repetitive detailed inspections and corrective actions for damage found between frame 48 and frame 54 on the right-hand side of the fuselage. An optional modification is provided to terminate the need for repetitive inspections.

Mar 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A300-600

EASA AD 2020-FATA-01020A-04

NOT ADOPTED - EASA DECISION ATTACHED

NOT ADOPTED - EASA DECISION ATTACHED is an Airworthiness Directive issued by the Federal Air Transport Agency of the Russian Federation on 2020-03-11. It applies to RRJ-95 aircraft with specific door arm part numbers and manufacturing serial numbers from 95007 to 95179. The directive addresses issues with the Emergency exit door and emergency escape slide system, focusing on the automatic door opening system EPAS.

Mar 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtIrkut Corporation Jsc RRJ-95RRJ-95

EASA SIB SW-20-01

Robinson R44 and R66 Helicopters - Electrical Power System - Battery Electrolyte Leakage

The Special Airworthiness Information Bulletin SAIB: SW-20-01 is an FAA informational bulletin addressing potential electrolyte leakage issues in the electrical power systems of Robinson R44 and R66 helicopters. The bulletin specifically concerns certain lead acid batteries manufactured by Concorde Battery, Inc., identified by Robinson part numbers B237-4 for the R44 and B237-7 and B237-8 for the R66 models. It informs operators about the leakage risk without mandating corrective action through an airworthiness directive.

Mar 11, 2020
Safety Information BulletinMaintenanceSafety Mgmt

EASA AD 2020-0055

SUPERSEDED BY EASA AD 2022-0071

EASA Airworthiness Directive 2020-0055 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting CFM International LEAP-1B engines installed on aircraft including Boeing 737-8 and 737-9 models. It mandates updated maintenance tasks, life limits, and software modifications to ensure continued airworthiness and address safety concerns related to high pressure turbine structures, rotor disc anomalies, bearing failures, and engine control software. The directive consolidates and supersedes previous ADs related to these engines.

Mar 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtCFM International LEAP-1BBoeing 737-8Boeing 737-9

EASA AD 2020-0054

SUPERSEDED BY EASA AD 2023-0199

EASA Airworthiness Directive 2020-0054 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A330-941 aeroplanes. It mandates repetitive operational tests of the hydraulic locking function of the spoiler servo control (SSC) units installed on the blue and yellow hydraulic circuits to ensure continued safe flight control. This directive addresses a failure mode related to a sheared seal on the blocking valve of the SSC that could reduce aircraft control during engine-out takeoff conditions.

Mar 11, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A330Airbus A330-941

EASA AD 2020-0052

Fuselage — Satellite Communications Antenna Doubler — Inspection / Replacement

EASA Airworthiness Directive 2020-0052 is an airworthiness directive affecting Airbus A319 aeroplanes, specifically models A319-111 through A319-133 with certain exceptions. It mandates inspection and replacement of the satellite communications (SATCOM) antenna doubler on the fuselage to address potential structural integrity issues. The directive applies to aircraft without specific Airbus modifications or service bulletin embodiments that mitigate the issue.

Mar 10, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A319

EASA AD US-2020-04-11

Fuselage - Upper Skin Lap Splice - Inspection

The Federal Register Volume 85, Number 46 Airworthiness Directive 2020-04-11 is a final rule issued by the FAA addressing certain Boeing 747-400 series airplanes. It mandates repetitive low frequency eddy current (LFEC) and high frequency eddy current (HFEC) inspections of the fuselage upper skin lap splice to detect fatigue cracks. The directive includes required on-condition repair actions to maintain structural integrity.

Mar 10, 2020
Airworthiness DirectiveMaintenanceSafety MgmtBoeing 747Boeing 747-400

EASA AD 2020-0053

Nacelles / Pylons — Engine Pylon Nose Fire Seals — Inspection / Replacement

EASA Airworthiness Directive 2020-0053 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A320-271N, A321-271N, A321-271NX, and A321-272N aeroplanes. It addresses inspection and replacement requirements for engine pylon nose fire seals with Part Number D0003109300000 to ensure firewall integrity. The directive mandates a detailed inspection and corrective actions to prevent potential loss of fire protection in case of an engine fire.

Mar 10, 2020
Airworthiness DirectiveMaintenanceSafety MgmtAirbus A320Airbus A321Airbus A320-271NAirbus A321-271NAirbus A321-271NXAirbus A321-272N

EASA AD CF-2020-03

Fuel System - Primary Ejector Fuel Feed Flexible Hoses Inner Tube Cracking

The Canadian Airworthiness Directive CF-2020-03 addresses cracking in the inner tube of primary ejector fuel feed flexible hoses on Bombardier aircraft models CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 within specified serial number ranges. This directive mandates replacement of affected flexible hoses that may have a thinner-than-required Teflon lining, which can lead to fuel leaks and potential engine flameouts. The directive aims to ensure continued safe operation by mitigating fuel system failures related to these components.

Mar 9, 2020
Airworthiness DirectiveMaintenanceSafety MgmtMHI RJ Aviation CL-600 (Regional Jet)Bombardier CL-600-2C10Bombardier CL-600-2C11Bombardier CL-600-2D15Bombardier CL-600-2D24Bombardier CL-600-2E25

EASA AD 2020-0048

SUPERSEDED BY EASA AD 2020-0197

EASA Airworthiness Directive 2020-0048 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Leonardo S.p.A. AW169 and AW189 helicopters. It addresses inspection, checking, and modification requirements related to the tail rotor servo actuator and duplex bearing to prevent potential loss of helicopter control. The directive includes repetitive inspections, thermal strip installations, and reporting obligations to ensure continued airworthiness.

Mar 6, 2020
Airworthiness DirectiveMaintenanceSafety MgmtLeonardo S.P.A. Helicopters AW169Leonardo S.P.A. Helicopters AW189Leonardo AW169Leonardo AW189

EASA AD 2020-0046

Engine Fuel & Control — Full Authority Digital Engine Control B / Digital Engine Control Unit — Inspection / Replacement

EASA Airworthiness Directive 2020-0046 is an airworthiness directive addressing SAFRAN Helicopter Engines ARRIEL 2C and 2S1 engines, commonly installed on Airbus Helicopters AS 365 N3 and Sikorsky S-76C helicopters. The directive focuses on inspection and replacement of Full Authority Digital Engine Control B (FADEC B) digital engine control units (DECUs) due to identified defects. It mandates replacement of affected FADEC B DECU units to ensure continued safe operation of the engines.

Mar 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtSafran ARRIEL 2Airbus Helicopters AS 365 N3Sikorsky S-76C

EASA AD 2020-0045

Fuel — Fuel Pressure Sensor — Inspection / Replacement

EASA Airworthiness Directive 2020-0045 is an airworthiness directive addressing the Pipistrel Vertical Solutions Virus SW 121 aeroplanes, specifically serial numbers VSW1210001 to VSW1210041. It mandates inspection and replacement of the fuel distribution block, Rotax Part Number 851328, associated with the fuel pressure sensor to prevent fuel leakage. The directive includes instructions for inspection, replacement, and modification of the installation to ensure continued airworthiness.

Mar 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtPipistrel Vertical Solutions D.O.O. Virus SWPipistrel Vertical Solutions Virus SW 121

EASA AD US-2020-03-16

Fuselage - Carry-Thru Spar Lower Cap - Inspection

Federal Register Volume 85, Number 35 (AD 2020-03-16) is a final rule airworthiness directive issued by the FAA addressing Textron Aviation Inc. Models 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, and T210M airplanes. It mandates inspections and corrective actions for the carry-thru spar lower cap due to fatigue cracking initiated by corrosion pits, which have caused in-flight structural failures. The directive also requires application of protective coatings and reporting inspection results to the FAA.

Mar 4, 2020
Airworthiness DirectiveMaintenanceSafety MgmtTextron Aviation 210 (Centurion)Textron Aviation 210GTextron Aviation T210GTextron Aviation 210HTextron Aviation T210HTextron Aviation 210JTextron Aviation T210JTextron Aviation 210KTextron Aviation T210KTextron Aviation 210LTextron Aviation T210LTextron Aviation 210MTextron Aviation T210M